Scientific and Technical Aerospace Reports, 29. sējums,1-3. izdevumsScientific and Technical Information Office, National Aeronautics and Space Administration, 1991 |
No grāmatas satura
1.–5. rezultāts no 100.
3. lappuse
... given . The Ga AEED device is concluded to be of not good enough quality for fair comparison to the silicon AEED . ESA N91-10017 # Institut Franco - Allemand de Recherches , Saint - Louis ( France ) . MEASUREMENT OF AIR ENTRAINMENT BY A ...
... given . The Ga AEED device is concluded to be of not good enough quality for fair comparison to the silicon AEED . ESA N91-10017 # Institut Franco - Allemand de Recherches , Saint - Louis ( France ) . MEASUREMENT OF AIR ENTRAINMENT BY A ...
7. lappuse
... given by a set of real time logic formulas ( rules ) . A modified rule to permit the preemption of low priority real time processes is proposed . ESA 05 AIRCRAFT DESIGN , TESTING AND PERFORMANCE Includes aircraft simulation technology ...
... given by a set of real time logic formulas ( rules ) . A modified rule to permit the preemption of low priority real time processes is proposed . ESA 05 AIRCRAFT DESIGN , TESTING AND PERFORMANCE Includes aircraft simulation technology ...
9. lappuse
... given and the progress achieved in the fields of performance , flying qualities , noise and vibrations , weight , reliability and safety is assessed . Studies for increasing the aircraft's capabilities are described and a prospective ...
... given and the progress achieved in the fields of performance , flying qualities , noise and vibrations , weight , reliability and safety is assessed . Studies for increasing the aircraft's capabilities are described and a prospective ...
12. lappuse
... given . The characteristics of operation of several turbines and their installation in ships are described . Suggestions for turbine power increase are given . ESA N91-10070 # Rolls - Royce Ltd. , Bristol ( England ) . TECHNOLOGY UPDATE ...
... given . The characteristics of operation of several turbines and their installation in ships are described . Suggestions for turbine power increase are given . ESA N91-10070 # Rolls - Royce Ltd. , Bristol ( England ) . TECHNOLOGY UPDATE ...
14. lappuse
... given cross flow plane . Further analysis of the three dimensional solution indicated that these slight lateral pressure gradients lead to negligible secondary flows , except within a small region in the corners within the boundary ...
... given cross flow plane . Further analysis of the three dimensional solution indicated that these slight lateral pressure gradients lead to negligible secondary flows , except within a small region in the corners within the boundary ...
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Citi izdevumi - Skatīt visu
Bieži izmantoti vārdi un frāzes
A17 CSCL Abstr aerodynamic aeroelastic Aeronautics and Space Aerospace AGARD AGARD/Scientific Publications Executive Air Traffic Handling airfoil algorithm alloys Ames Research Center analysis Atmospheric Author cirrus cirrus clouds cloud composite Computational Fluid Dynamics Contract Copyright Avail Dept described developed effects electron energy Engineering ENGLISH summary equations evaluation experimental field flow function grid Guidance of Aircraft HC/MF A03 CSCL heat Includes Inst interaction investigated Langley Research Center laser lidar magnetic measurements mechanical Meteorological Satellite Center method Microfilms Order NASA National Aeronautics National Lab Nationals requests available Navier-Stokes equations Netherlands Non-NATO Nationals requests nonlinear NTIS HC/MF A03 numerical observed operating optical parameters performance Ph.D plasma Plasma Physics Prediction presented primary document problems Propulsion Report Sandia National Labs simulation solar Space Administration spacecraft superconducting surface techniques Technology temperature thermal Thesis turbulence Univ Universiteit Twente velocity wave wind windshear
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